Another hypothesis for everyone to chew on.
"Mercedes are running their engine leaner than Renault and Ferrari."
1. MB clearly have a power advantage and therefore a thermal efficiency advantage.
2. A lot of people are suggesting that Mercedes are using a larger turbine. I don't know what the evidence for this is but if true, a larger turbine suggests a higher mass flow, higher boost and leaner mixture.
3. It is apparent that Mercedes are able to charge the ES more rapidly and run at maximum output for longer before needing to recharge. To do this they must be harvesting more energy from their turbine (MGUK). This suggests a higher pressure ratio and mass flow through their turbine.
Another way to look at this is to consider the PU as a gas turbine engine with a recip' engine as the combustion chamber. Gas turbines increase in efficiency as the PR is increased. (This is analogous to increasing the CR and ER in a recipe engine). The limit on PR is the temperature exiting the combustion chamber and entering the turbine. The turbo compound engine extends this limit by performing a lot of the compression and expansion in a recip' cylinder where the peak pressure and temperature is very brief (just after TDC) and intermittent (combustion chamber components are cooled by the fresh charge for a large percentage of the cycle). Evidence from the Napier Nomad and the Garrett helicopter proposal indicates that best efficiency coincides with very high PR in the turbo machinery (of the order of 10:1) and moderate compression ratios in the recip' machinery. In the Garrett paper (http://ntrs.nasa.gov/archive/nasa/casi. ... 001160.pdf) PR is 10.3 on the intake side and 9.3 on the exhaust side. Turbine output is 32% of ICE crankshaft power (24% of total power) which is equivalent to about 150kW
The situation in the F1 PU is quite different. Excess power generated in the turbine can only be consumed at the rate of 120kW (MGUK limit) the rest must go to storage. To maximise the continuous power available to the wheels, it would be better to reduce the turbine power in favour of higher crankshaft power from the recip' (by reducing PR) - even though this would result in lower efficiency and therefore lower total power. Other considerations limiting PR include small electrical losses in converting turbine power to electricity in the MGUK and back to work in the MGUH and probably also lean combustion limits in the SI recip'.
I think it is reasonable to guess that MB has similar crankshaft power but higher turbine power compared to the other teams. The obstacles MB may have overcome to achieve this include:
- Extending stable combustion to leaner mixtures. Possible methods include - higher intake temp for stable combustion of homogeneous mixtures (see Honda researchhttp://www.greencarcongress.com/2014/04 ... -hlsi.html), extending stratified charge to higher (10,500+) rpm.
- Operating at a higher PR without significant reduction in CR. Detonation control by lean mixture and/or stratified charge.
- Reduced inter-cooling would improve combustion stability as stated above but will also increase turbine power.